ES2388104B1 - SUSTAINER, PROPULSOR AND STABILIZER SYSTEM FOR AIRCRAFT AND VERTICAL LANDING AIRCRAFT. - Google Patents

SUSTAINER, PROPULSOR AND STABILIZER SYSTEM FOR AIRCRAFT AND VERTICAL LANDING AIRCRAFT.

Info

Publication number
ES2388104B1
ES2388104B1 ES201000248A ES201000248A ES2388104B1 ES 2388104 B1 ES2388104 B1 ES 2388104B1 ES 201000248 A ES201000248 A ES 201000248A ES 201000248 A ES201000248 A ES 201000248A ES 2388104 B1 ES2388104 B1 ES 2388104B1
Authority
ES
Spain
Prior art keywords
aircraft
sustainer
propulsor
stabilizer system
vertical landing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
ES201000248A
Other languages
Spanish (es)
Other versions
ES2388104A1 (en
Inventor
Saiz Manuel Munoz
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to ES201000248A priority Critical patent/ES2388104B1/en
Priority to US13/392,674 priority patent/US9889928B2/en
Priority to PCT/ES2010/000204 priority patent/WO2011023834A1/en
Publication of ES2388104A1 publication Critical patent/ES2388104A1/en
Application granted granted Critical
Publication of ES2388104B1 publication Critical patent/ES2388104B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • B64C27/30—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with provision for reducing drag of inoperative rotor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0025—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
ES201000248A 2009-08-26 2010-02-11 SUSTAINER, PROPULSOR AND STABILIZER SYSTEM FOR AIRCRAFT AND VERTICAL LANDING AIRCRAFT. Expired - Fee Related ES2388104B1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
ES201000248A ES2388104B1 (en) 2010-02-11 2010-02-11 SUSTAINER, PROPULSOR AND STABILIZER SYSTEM FOR AIRCRAFT AND VERTICAL LANDING AIRCRAFT.
US13/392,674 US9889928B2 (en) 2009-08-26 2010-05-05 Lift, propulsion and stabilising system for vertical take-off and landing aircraft
PCT/ES2010/000204 WO2011023834A1 (en) 2009-08-26 2010-05-05 Lift, thrust and stabiliser system for vertical take-off and landing aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES201000248A ES2388104B1 (en) 2010-02-11 2010-02-11 SUSTAINER, PROPULSOR AND STABILIZER SYSTEM FOR AIRCRAFT AND VERTICAL LANDING AIRCRAFT.

Publications (2)

Publication Number Publication Date
ES2388104A1 ES2388104A1 (en) 2012-10-08
ES2388104B1 true ES2388104B1 (en) 2013-09-06

Family

ID=46853401

Family Applications (1)

Application Number Title Priority Date Filing Date
ES201000248A Expired - Fee Related ES2388104B1 (en) 2009-08-26 2010-02-11 SUSTAINER, PROPULSOR AND STABILIZER SYSTEM FOR AIRCRAFT AND VERTICAL LANDING AIRCRAFT.

Country Status (1)

Country Link
ES (1) ES2388104B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2684859B1 (en) * 2017-03-31 2019-08-20 Saiz Manuel Munoz Lifting and stabilization system for UAVs or drones by means of electrically operated oscillating fans or fins

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1662406A (en) * 1928-01-10 1928-03-13 Elmer H Thompson Airplane
FR816813A (en) * 1936-04-22 1937-08-18 Flying device
IT1297108B1 (en) * 1997-12-10 1999-08-03 Franco Capanna SYSTEM FOR THE TRANSFORMATION OF A SELF-SUPPORTED HORIZONTAL FLIGHT AIRCRAFT INTO AN INTEGRATED, HYBRID TAKE-OFF AIRCRAFT
US6622962B1 (en) * 2002-04-29 2003-09-23 Bruce D. White Fixed wing aircraft having powered rotor VTOL capability with rotor blades stowable during horizontal flight
ES2275370B1 (en) * 2004-03-05 2008-05-01 Industria Helicat Y Alas Giratorias, S.L. METHOD OF OPERATION OF A CONVERTIBLE AIRCRAFT.
ES2293818B1 (en) * 2006-02-09 2009-02-16 Manuel Muñoz Saiz SUSTAINER AND PROPULSOR SYSTEM FOR AIRCRAFT AND VERTICAL LANDING AIRCRAFT.
ES2288083B1 (en) * 2005-07-20 2008-10-16 Manuel Muñoz Saiz SUSTAINING PROVISION FOR AIRCRAFT AIRCRAFT AND VERTICAL LANDING.
ES2289932B1 (en) * 2006-07-03 2009-03-01 INSTITUTO NACIONAL DE TECNICA AEROESPACIAL "ESTEBAN TERRADAS" AIRCRAFT WITH CONVERTIBLE FLIGHT SYSTEM.
WO2009047376A1 (en) * 2007-10-11 2009-04-16 Munoz Saiz Manuel Propulsion and lifting system and method for vtol craft and aircraft

Also Published As

Publication number Publication date
ES2388104A1 (en) 2012-10-08

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Legal Events

Date Code Title Description
FD2A Announcement of lapse in spain

Effective date: 20210915